US3336181A - Molding apparatus and process for making the same - Google Patents
Molding apparatus and process for making the same Download PDFInfo
- Publication number
- US3336181A US3336181A US53743666A US3336181A US 3336181 A US3336181 A US 3336181A US 53743666 A US53743666 A US 53743666A US 3336181 A US3336181 A US 3336181A
- Authority
- US
- United States
- Prior art keywords
- layer
- vacuum
- porous
- porous metal
- mold
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/26—Component parts, details or accessories; Auxiliary operations
- B29C51/30—Moulds
- B29C51/36—Moulds specially adapted for vacuum forming, Manufacture thereof
- B29C51/365—Porous moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
- B29C33/3814—Porous moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/024—Thermal pre-treatments
- B29C66/0242—Heating, or preheating, e.g. drying
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S425/00—Plastic article or earthenware shaping or treating: apparatus
- Y10S425/06—Vacuum
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249981—Plural void-containing components
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249987—With nonvoid component of specified composition
- Y10T428/24999—Inorganic
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249987—With nonvoid component of specified composition
- Y10T428/249991—Synthetic resin or natural rubbers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/10—Scrim [e.g., open net or mesh, gauze, loose or open weave or knit, etc.]
- Y10T442/102—Woven scrim
- Y10T442/152—Including a free metal or alloy constituent
Definitions
- the present invention relates to a vacuum molding apparatus and a process for making the same, and more particularly concerns a low cost, lightweight porous metal mold for use in vacuum forming sheet materials.
- thermoplastic sheet materials are many and varied. In many vacuum forming operations, there is Ia definite problem in preventing or eliminating air entrapment between the surface of the hot, plastic sheet and the surface of the mold.
- thermoplastic sheet-like materials are made underv pressure by means of pressure rolls, press plates, or vacuum bags.
- the material is sandwiched between two surfaces and pressed to obtain the desired printed design from one or both surfaces.
- the trapping of air in deep grooves or pockets of the design embossed on the stock is only one of numerous problems inherent in the technique, especially when very thin or expanded stock is being used.
- Other problems include the tendency of the hot stock to collapse while being passed through the nip of the rollers, the difficulty in maintaining accurate thickness gauge controls for complete and uniform embossing,
- the present invention contemplates and has as its primary object the provision of a light weight, low cost porous metal vacuum mold offering both high structural strength and a high rate of air flow through the porous metal molding surface. It is a further object of this invention to provide a high strength porous metal vacuum mold in which the thickness of metal between the iracuum attachment and the heated stock is not so great as to interfere with the rate of air flow through the porous metal structure necessary to eliminate air entrapment between the surface of the hot plastic sheet and the surface of the mold.
- Still another object of this invention is to provide porous metal vacuum embossing rolls which not only prevent the entrapment of air between the rolls and the material being embossed, but also have none of the disadvantages common to embossing systems in which the material to be embossed is sandwiched between two surfaces and pressed to obtain the desired imprinted design.
- Another object of this invention is to provide a method for making the above-described porous metal vacuum molds, embossing rolls, embossing plates, etc.
- a porous vacuum mold comprising a composite of a first layer of porous metal and a second layer of metal, the two layers being partially in contact and partially separated by channels communicating with a vacuum source and all surfaces of the composite except for the molding surface of the rst layer being covered with an air-impermeable sealer.
- the channels of the mold are formed by burning a combustible fiber between the two layers so as to leave open, distinct and well defined channels therebetween.
- FIG. 1 is a front view showing the application of a first layer of porous metal on a flat embodiment mandrel
- FIG. 2 is a perspective view showing the application of a second layer of porous metal on top of a fabric layer over the first porous metal layer;
- FIG. 3 is a sectional front view showing, prior to heating in the oven, the :composite formed of the second porous metal layer, the fabric layer, the first layer and the mandrel;
- FIG. 4 is a sectional front View of a segment of the composite after removal of the mandrel and application of a sealer layer;
- FIG. 5 is a perspective view of the finished mold and the texture of the top surface thereof;
- FIG. 6 is a sectional front view of the finished mold and the thermoplastic sheet material to be molded
- FIG. 7 is a sectional perspective View showing the application of a first layer of porous metal on a roll embodiment mandrel
- FIG. 8 is a sectional perspective view of the structure of the fiber layer (of non-interconnected longitudinal fibers) over the first porous metal layer and its relation with a roll ring;
- FIG. 9 is a sectional perspective view showing the application of a second layer of porous metal on top of the fiber layer prior to heating of the oven;
- FIG. l is an axially exploded sectional perspective view of the finished mold mounted for rotation on a shaft;
- FIG. 11 is a sectional perspective view of the finished mold in operation
- FIG. 12 is a front and top view of a commutator ring
- FIG. 13 is a front and top view of a roll ring
- FIG. 14 is a sectional front view of a roll embodiment produced by the reverse process.
- FIG. 15 is. a sectional front view of the fiat embodiment produced by the reverse process.
- the substantially fiat mandrel '10 is suitably a plaster form having the desired surface texture and configuration of the surface of the molded product, i.e., it is a positive of the surface of the desired product.
- the texture of the mandrel shown consists of a series of grooves 11 and ridges 12; however, choice of the texture and, for that matter, the configuration of the mandrel are matters of choice depending upon the specific product desired.
- the mandrel 10 is larger than the desired product, the desired product being no longer than the distance between the trim edges 13. These trim edges 13 are either grooves or ridges which define the periphery of the molding area and facilitate the removal of the final product from the mold.
- a substantially fiat first layer of porous metal is applied over the top surface of the mandrel 10 in such a way as to conform to the surface of the mandrel 10.
- This first layer 15 of porous metal is very thin, preferably ranging in depth from about V16 inch to about 1A; inch, and is made up of particles of metal lightly mechanically bonded together. It is very porous and will later serve as the molding surface of the vacuum forming mold.
- the first layer 15 of porous metal may be applied over the entire surface of the mandrel 10 in the form of molten metal by a flame sprayer 16 or by any of the other conventional techniques for forming porous metal layers, such as applying powdered metals or sintering, including the techniques and sprayers described in Modern Plastics, supra, or any of the following U.S. Patents 2,754,225; 2,772,920; 2,784,029; 2,868,667-provided that such technique does not cause undue weakening of the plaster form being used as a mandrel 10.
- a plaster form as the mandrel material affords certain advantages to be pointed out later, other conventional mandrel materials may be used such as wood, plastic, etc. Where needed, the mandrel 10 should be provided with a release coat to facilitate its subse'quent removal from the first layer 15 of porous metal.
- a suitable release coat for a plaster form is a light coating of nylon deposited from a solution of nylon in alcohol, but other conventional release coats may also be used such as silicone releases, etc.
- the fiame sprayer 16 While aluminum is the preferred porous metal because of its low cost, ease of handling, relatively low temperature requirement for spraying, and the resultant lower weight of the end product, other metals such .as low melting steels, bronze, copper, nickel and various alloys may be utilized. When the first layer is applied by the spraying of essentially molten metals, the fiame sprayer 16 must be capable of heating materials to the proper temperature for such spraying.
- a fabric 20 is placed over and in contact with the entire surface of the first layer 15 of porous metal.
- the fabric 20 extends over and conforms to the entire top surface. Placement of the fabric can be facilitated by wetting the fabric so that it can be contoured to follow closely the surface.
- the fabric 20 is suitably an open weave combustible fabric, typically a net having approximately 2 to 8 warp and woof (fill) threads per inch, prefer-ably 3 to 4 threads per inch. Each thread has a diameter of from approximately 1A'- to 1/64 inch, preferably about 1/32 inch, It should be recognized that these limitations are not critical, so long as the fabric is loosely woven.
- the fabrics used in this invention must be of the type which can be destroyed at temperatures below that which will adversely affect the structure of the porous metal. It is preferred that the material be the type which tends to char or burn readily so as to leave channel voids in the porous metal structure.
- Cotton, wool and vegetable fiber material, such as woven paper fabrics are among the preferred materials while synthetic fibers such as nylon (polyamides) are not as desirable because (l) they tend to expand on exposure to the high temperature later required, thereby putting a strain on the mold, and (2) they tend to become fluid in such a way as to clog the walls of the passageways to be formed, thereby reducing the effectiveness of the vacuum system.
- a substantially flat second layer 25 of porous metal is then applied, e.g., sprayed, over the entire surface of the fabric 20 and into the interstices thereof, so as to contact the portions of the first layer 15 not directly covered yby the fabric 20.
- the second layer 25 of porous metal is sprayed to a thickness ranging in minimum thickness from about 3A@ to 1A inch.
- the result is a total sprayed metal layer (made up of layers 15 and 25) of Iapproximately 1A; to Vs inch minimum thickness having embedded therein an open weave net fabric layer.
- the composite structure now consists of a plaster form 10, a first sprayed metal layer 15, and open weave combustible fabric 20, and a second sprayed porous metal layer 25.
- This composite structure is then placed in an oven 30 and heated at 600 to 750 F. for four hours.
- the temperature and time of this heating step will vary with the particular materials which compose the composite structure. The exact duration and temperature will depend on what is necessary to accomplish the purposes of the heating step.
- the heating step accomplishes the following objectives: (a) the fabric is burned or reduced to easily removable ash within the porous mold structure leaving defined, open passageways; (b) the water of hydration present in the plaster is removed at this temperature, thereby weakening the plaster and facilitating later removal of the plaster from the first layer 15 of sprayed metal; and (c) the metal layers (without liquifying) become stress relieved, thereby eliminating internal stresses, and form a strong self-supporting structure around the passageways.
- the composite structure is then removed from the oven and the plaster mold is broken away from the first layer 15 of porous metal to reveal a textured molding surface of ridges 43 and grooves 44.
- the remaining composite consists of the first layer 15, the second layer 25, and the channels 45 therebetween which were created by combustion of the fabric layer 20.
- the sides and the back surface of the remaining composite i.e., the exposed outer areas of the remaining composite which were not in contact with the mandrel 10) are then sealed so as to render them air impermeable and to reinforce the remaining composite permitting it to be handled and used without damage thereto.
- sealing was accomplished by coating the sides and back surface of the remaining composite with a sealer layer 40 of epoxy resin and glass cloth; however, other conventional materials and techniques for sealing surfaces (strengthening them and rendering them air impermeable) may be used instead of, or in addition to, the layer 40 of epoxy resin and glass cloth.
- vacuum holes 51 are created along the periphery of the molding area (comprised of ridges 43 and grooves 44), but outside of the trim line formed by the trim edges 13, i.e., in 4the scrap area of any thermoplastic sheet formed over the mold surface.
- the -vac holes 51 extend only through the first layer and may be made by drilling, as with a 50 gauge wire drill, through the first layer 15 of porous metal or by other conventional means well known in the art.
- the vac holes 51 are used to obtain a quick initial pull down of the material to be molded (to speed up the molding process), but are not an essential part of the structure.
- a large bore and preferably thick-Walled tube 50 is attached to the back or rear surface of the porous -rnold structure and makes an air-impermeable contact with the sealer layer 40.
- the large bore hole 60 extending through Ithe second layer 25 is suitably made by drilling a W16 inch hole through the second porous metal layer, or by masking portions of the volume to be sprayed with metal to form the second layer.
- the large bore hole 60 communicates with the tube 50 Vand the channels 45 resulting from the combustion of the fabric layer 20.
- the large bore tube 50 is fitted with switching means (not shown) for connecting the large bore hole 60 alternately with a vacuum source (not shown) and a source of greater pressure (not shown)preferably -a-t least atmospheric-as desired for the molding operation and sheet removal operation, respectively.
- the large bore hole 60 ⁇ and large bore tube 50 act as communicating means Ibetween the vacuum or pressure source and the channels; the first layer 15 of porous metal, in turn, acts as communicating means for vacuum or pressure between the channels and the top surface of the porous mold structure to prevent air entrapment and facilitate sheet removal.
- the large bore hole 60 directly communicates with several of the small vac holes 51 extending tothe top surface of the porous mold structure and communicates with others indirectly by means of the channels. There may be a single large bore hole 60l and large bore tube 50 or there may be a plurality of them. V
- a sheet 61 -composed of unvulcanized rubber or a thermoplastic, heat-softenable plastic heated a few degrees beyond its softening point by heat lamps (not shown), is held within a rectangular holding clamp or frame 62 (say of metal).
- the frame 62 is lowered or the mold is raised to thereby cause the sheet 61 to contact the top or molding surface of the porous mold structure, the molding surface having been preheated by heat lamps (not shown) to about 140 F. to prevent premature cooling of the sheet 61 before molding.
- the vacuum source creates a vacuum immediately above the molding surface so as to pull the hot plastic sheet 61 into close contact with the molding surface, first contact occurring around the outside edge of the trim line formed by the trim edges 13 as this area is closest to the direct communication of the vacuum acting directly on the sheet 61 through the vac holes 51.
- the vacuum action takes place through the channels and, in turn, produces a vacuum at the surface ofthe top layer 15 of porous metal, thereby forcing the hot plastic sheet 61 into intimate contact with the top surface of the first layer 15 of porous metal.
- the Vac holes 51 are therefore useful in causing the original seal of the plastic sheet 61 to the top surface of the first layer 15 of porous metal, so that the vacuum action through the rst layer 15 is especially efficacious.
- the vac holes 51 may be connected to a vacuum source dis tinct and separate from the vacuum source acting through the passageways.
- the molded product may be used as a mat for automobiles, a cushion surface, a section of the surface for luggage, etc.
- the surface of the porous mold structure illustrated in the drawings is relatively flat, but for specific applications it may be of any desired form and configuration.
- second layer 25 is preferably composed of porous metal, like the first porous metal loyer 15, and although the fabric layer 20 preferably is composed of a lattice of fibers so that the channels resulting from combustion of the fibers are interconnecting (rather than not directly interconnecting as when the fibers of the fabric layer are all substantially parallel), the second layer 25 may be non-porous and/ or non-metallic and some or all of the channels 45 may be other than directly interconnecting.
- a second layer 25 which is composed not of a porous metal, but rather either of a non-porous metal or of a resin of high distortion temperature, such as an epoxy resin, which will not itself burn or distort during combustion of the fabric layer 20, the bers of which have a low ignition point relative to the distortion temperature of the resin.
- the second layer 25 is composed of an air-impermeable (non-porous) material, be it metal or high distortion temperature resin, it is essential that the second layer 25 does not completely encapsulate the fibers of the fabric layer 20 or the passageways formed by combustion of the fibers will not communicate with the molding surface of the first layer 15 or porous metal.
- the second layer 25 is composed of such an airimpermeable non-porous material, it can serve both as a second layer 25 and as the portion of the sealer layer 40 which, in the other embodiments, surrounds the exposed outer areas of the second layer 25.
- a non-porous second layer 25 may interfere with the vacuum draw of certain channels, e.g., those formed at the location of the alternate (lower) warp threads, which it partially surrounds, thereby causing irregularities in the vacuum on the top surface of the porous mold structure.
- the porous mold structure having two porous metal layers is thereforeL preferred for most, but not all, applications as it allows any portion (top or bottom) of any channel to suck air from the mold interior so as to produce a uniformly distributed vacuum of constant strength over the molding surface.
- the mandrel 10 used is typically, a reinforced, substantially cylindrical plaster shell of rigid form having .an interior surface with a positive of the desired texture of ridges 12 and grooves 11 on it.
- a mandrel 10 may be formed by casting around an existing embossing roll a continuous seamless cylindrical sleeve of an elastic material capable of capturing and retaining the desired texture of the roll, e.g. vinyl plastisol, silicone and polysulfide rubber, etc.
- the continuous cylindrical sleeve may also be made flat and later seamed to form a cylinder where the design or texture lends itself to incorporating the seam as part of the design or later editing it out.
- the sleeve is then removed from the embossing roll and pulled over a disposable frame with the textured side facing outwards.
- a reinforced plaster shell may then be poured lover the textured surface to obtain a rigid form having the interior surface with the desired texture.
- the disposable frame and the plastisol (or other) sleeve are then removed from the interior of the plaster.
- the inner surface of the hollow plaster mandrel 10 is then sprayed with metal, utilizing a flame sprayer 16, to form a substantially cylindrical first layer 15 of porous metal preferably approximately l/l inch thick.
- Icombustible fibers preferably of from 1/32 to 1/16 inch in diameter
- the fibers 20 lie approximately 1A inch apart and may be held down to the first layer 15 with a small amount of combustible cement (not shown), such as an unloaded rubber cement, an animal glue or a starch solution, which degrades or tends to disintegrate at the stress relieving temperatures used.
- Either or both ends of the mandrel 10 are outfitted with prefabricated annular roll rings(s) 130 having extending therethrough roll ring channels or holes 131 (as shown in FIG. 13) aligned along the same longitudinal lines as the fibers 20. Each hole has a slightly greater diameter than that of the fibers.
- the ends 81 of the fibers 20 are then pulled through roll ring channels or holes 131 and knotted or fastened to each other, there being one hole for each fiber end 81.
- a substantially cylindrical second layer of porous metal (preferably, though not necessarily, porous) is applied, as by a flame sprayer 16, over and between the fibers so as to contact the exposed portions of the rst layer 15 (the portions not covered by the fibers 20) and the inner sides of the roll rings(s) 130 until the combined minimum thickness of the first and second layers 15, 25 is approximately 1/2 inch.
- the entire assembly is then heater in an oven to approximately 650 F.
- first and second layers 15, 25 and roll ring(s) 130 is slightly warmed to facilitate its placement over a nonporous, rotatable roll shaft of suitable diameter which acts las an air-impermeable sealer for the second layer 25 (see FIGS. l0-1l). If only one end ⁇ of the mold has been sealed by the use of a non-porous rool ring 130, the other end is sealed with an aim-impermeable sealer layer.
- the smooth inner face 121 of a non-porous ring commutator 120 is snugly fitted in a face-to-face relationship against the smoothed outer face 135 of the roll ring 130.
- the roll ring 130 engages one end of the roll for rotation therewith; the outer commutator ring 120 is stationary and fixedly connected to base 112.
- the inner face 121 of commutator ring 120 has two separate recessed grooves 122, 123.
- Recess groove 122 is attached to a vacuum source (not shown) by the tube 102; while recess groove 123 is attached to a source of lesser vacuum (not shown) by tube 103 (eg.
- Recess grooves 122, 123 are located for communication with the roll ring channels, i.e., holes 131, which, in turn, communicate with the channels 45 formed by the combustion of the fibers.
- the roll embodiment so prepared and assembled, as in FIG. l1, will emboss hot thermoplastic material 61 guided by rollers 105 over that portion of its surface to which a vacuum is applied via the internal channels during the vacuum phase, and the thermoplastic material embossed with ridges 46 and grooves 47 will then be removed from the embossing surface of the roll during the venting or pressure phase.
- the contact times under vacuum or pressure (venting) can be varied by changing the length of the commutator ring recess grooves 122, 123.
- the fixed commutator ring is positioned in a faceto-face, slidable air-tight manner against the rotating roll ring 130.
- certain of the holes 131 will be lined up with the recess groove 122 and, therefore, vacuum will be applied to sections of the roll connecting with those particular channels 45 aligned with said holes 131, thereby assisting the embossing.
- these channels 45 and their corresponding holes 131 will become lined up with the recess groove 123 and will be pressurized or vented to the atmosphere, thereby facilitating stripping of the embossed material from those sections of the roll.
- the Vacuum is applied to any section of the porous metal vacuum embossing roll only through approximately 270 or some analogous portion of its rotation and pressure or venting is applied during the remainder of the rotation cycle.
- This system of roll ring and commutator ring 120 in the roll embodiment therefore corresponds to the switching mechanism in the flat embodiment first described which connects the large bore tube 50 alternately to either a vacuum source or a pressure (or venting) source.
- passageways formed in the at embodiment may or may not be interconnecting
- the passageways formed in the roll embodiment are preferably not interconnecting as it is desired to apply, at any given instant, pressure (or venting) to one set of these channels and vacuum to another set of channels.
- the spider-type shaft is a rotatable roll shaft having a diameter considerably smaller than the inner surface of theV second layer 25 and radial or spider arms extending radially therefrom.
- each single hollow radial arm may be caused (as by the boring of appropriately located holes through the second layer) to communicate at the outer tip directly with the corresponding single open passageway and, at another point along its length, with a commutator ring of the type earlier described and shown in FIGS. 12 and 13 of the drawings.
- the pressures and Vacuums are distributed by the commutator system to the appropriate longitudinal hollow passageways by means of the hollow radial arms rather than through the roll rings 130, which may therefore be dispensed with.
- cooling means may be provided to accelerate the cooling and hardening of the hot plastic material after molding.
- Any conventional cooling means may be used, either external or internal to the mold.
- tubes for the conduction of water or forced air drafts may be located, for instance, in the second layer 25 of any embodiment or in the shaft 100 of the roll embodiment.
- the surface of the plaster mandrel contacting the first layer 15 may be smooth, i.e., without any grooves 11 or ridges 12, so that the molding area produced is smiliarly smooth.
- the first layer 1S may vbe engraved with the desired texture by standard engraving techniques. If the engraving solution plugs the porosity of the first layer 15, then the molding surface thereof may be blasted with water and/ or slightly etched with solvents to recapture the porosity.
- the process for building the mold may be reversed.
- a mandrel which may be a rotatable shaft 100 (equipped with journals and a water cooled interior) is blasted to receive and hold metal.
- the second layer 25A of metal is then applied, e.g., sprayedonto the blasted surface to a thickness of 1/s inch.
- Either the shaft 100 or the second metal layer 25A is non-porous (air-impermeable).
- Longitudinal fibers are fixed to the surface of the second layer 25A with a suitable combustible cement (not shown) such as animal glue or a starch solution.
- Roll rings 130 are fixed to the ends of the second layer A over the shaft 100 and the ends of the fibers 20 are fastened through holes 131.
- the first layer 15A of porous metal is sprayed over the fibers 20, the exposed areas of the second layer 25A of porous metal, and the roll rings 130 to obtain a completely smooth surface (or one that can be so smoothed) having approximately $66 inch of sprayed metal over the fibers.
- the whole assembly is then heated at 650 F. in an oven to anneal the metal layers 15A, 25A and also burn or char out the fibers 20.
- the outer or molding surface is next engraved with a negative of the desired texture of grooves 44 and ridges 43 by standard engraving technique methods, the molding surface being waterblasted and/or slightly etched to re-open the first layer 15A if the engraving solution plugs the porosity of the metal.
- the assembly is then equipped with a commutator 10V ring 120, which is attached to fixed base 112 and has separate recess grooves 122, 123 communicating, respectively, With vacuum and pressure sources by means of tubes 102, 103.
- the roll is then ready for use as described above.
- the procedure for the formation of the fiat embodiment may be reversed.
- the second layer 25A of porous metal is sprayed over a non-porous support 40A corresponding to thel sealer layer 40 (FIG. 6) at the base of the mold.
- a non-porous second metal layer may be applied over a release-treated removable surface.
- Woven or non-Woven fabric is applied over the second layer 25A.
- the first layer 15A is then sprayed over the fabric and exposed portions of the second layer 25A.
- the thickness of the first layer 15A is appropriately adjusted to allow for any diminution thereof due to the subsequent texturing by standard engraving techniques.
- a sealer layer 40B (corresponding to the sealer layer 40 (FIG. 6) at the edges of the mold) is applied around the edges of the first and second layers 15A, 25A.
- the vac holes 51 and large bore hole 60 are drilled, and large bore tube 50 is inserted and connected to vacuum and pressure sources.
- the mold is then ready for use as described above.
- an object comprising: a layer of porous metal having a shape-imparting surface and a back surface, a supporting layer of metal adjoining said back surface, a plurality of combustible fibers interposed between the adjacent surfaces of said layers, said layers being bonded together in the interstices between said fibers.
- an object comprising: a porous layer of sprayed metal having a shape-imparting surface and a back surface, a supporting layer of metal adjoining said back surface, a layer of open-weave combustible fabric interposed between said back surface and the adjoining surface of said supporting 3,336,181 11' 12 layer, said porous layer and said supporting layer being References Cited rrnly bonded together in the interstices of said open- UNITED STATES PATENTS weave fabric.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
Description
I Aug '15, 1967 v. A. FALKENAU ETAL 3,336,181
MOLDING APPARATUS AND PROCESS FOR MAKING THE ySAME Original Filed May 22, 1963 n 4 ShQtS-Sheet l .A T TORNEI.r
Allg- 15,1967 v. A. FALKENAU ETAL l 3,336,181
MOLDING APPARATUS AND PROCESS FOR MAKING THE SAME original Filed May 22, 1963 4 Sheets-Sheet 2 o n u o q n e u a n n a n Allg-A 15, 1967 v. A. FALKENAU ETAL 3,336,181
MOLDING APPARATUS ND PROCESS FOR MKING THE SAME 4 sheets-sheet :s
Original Filed May 22 ATTORNEY AUS 15. 1967 v. A. FALKENAU ETAL 3,336,181
MOLDING APPARATS AND PROCESS FOR MAKING THE SAME Original Filed May 22, 1.963
4 Sheets-Sheet 4 j (luna. f
AT TOR NEY United States Patent O 3,336,181 MULDING APPARATUS AND PROCESS FOR MAKING THE SAME Vernon A. Falkenau and Carl W. Church, Mishawaka, Ind., assignors to Uniroyal, Inc., a corporation of New 3 Claims. (Cl. 161-89) This application is a division of our copending application Ser. No. 484,043, filed Aug. 31, 1965, now Patent No. 3,293,737 which in turn is a division of our copending application Ser. No. 282,443, filed May 22, 1963, now Patent No. 3,262,159.
The present invention relates to a vacuum molding apparatus and a process for making the same, and more particularly concerns a low cost, lightweight porous metal mold for use in vacuum forming sheet materials.
The techniques and types of molds used in vacuum forming thermoplastic sheet materials are many and varied. In many vacuum forming operations, there is Ia definite problem in preventing or eliminating air entrapment between the surface of the hot, plastic sheet and the surface of the mold.
Many methods have been devised to overcome or minimize this problem, including the use of bleeder cords on the mold surface and small holes drilled in the mold surface. Each of these -approaches has definite limitations and some disadvantages. Bleeder cords tend to cause lines which are visible in the final product. The use of small holes drilled in the mold surface is very expensive as a large number of holes are required over the entire mold surface for even partial effectiveness. Furthermore, especially when the sheet material-s are being vacuum formed against a smooth or relatively smooth surface, these holes are visible, usually as a sprue, in the final product.
Recently, methods have been devised for making low cost porous metal structures through the use of techniques such as the spray metal technique. Some details of the construction and use of these porous metal structures as thermo-forming molds, as well as their advantages over the prior art, are described in Modern Plastics, vol. 39, No. 9, pp. 139 ff; (May, 1962). The difficulty inherent in the use of porous metal molds stems largely from the fact that, in order to provide a high strength vacuum mold, the porous metal must be so thick as to seriously interfere with the rate of air ow through r the porous metal structure, thereby reducing the vacuum to such a low value that the heated stock does not properly conform to the mold surface.
Presently, the molding or embossing of most thermoplastic sheet-like materials is done underv pressure by means of pressure rolls, press plates, or vacuum bags. In all cases, the material is sandwiched between two surfaces and pressed to obtain the desired printed design from one or both surfaces. Again, the trapping of air in deep grooves or pockets of the design embossed on the stock is only one of numerous problems inherent in the technique, especially when very thin or expanded stock is being used. Other problems include the tendency of the hot stock to collapse while being passed through the nip of the rollers, the difficulty in maintaining accurate thickness gauge controls for complete and uniform embossing,
3,336,181 Patented Aug. 15, 1967 cel the pulling and distortion of the fabric layer of a coated fabric as it passes through the pressure bite between nip rolls, the need for maintaining expensive back-up rolls, and the wasteful use of more material than is really necessary.
The present invention contemplates and has as its primary object the provision of a light weight, low cost porous metal vacuum mold offering both high structural strength and a high rate of air flow through the porous metal molding surface. It is a further object of this invention to provide a high strength porous metal vacuum mold in which the thickness of metal between the iracuum attachment and the heated stock is not so great as to interfere with the rate of air flow through the porous metal structure necessary to eliminate air entrapment between the surface of the hot plastic sheet and the surface of the mold.
It is still another principal object of this invention to provide porous metal vacuum rolls and plates which are of high strength and yet avoid the entrapment of air within any deep grooves and recesses of the stock.
Still another object of this invention is to provide porous metal vacuum embossing rolls which not only prevent the entrapment of air between the rolls and the material being embossed, but also have none of the disadvantages common to embossing systems in which the material to be embossed is sandwiched between two surfaces and pressed to obtain the desired imprinted design. i
Another object of this invention is to provide a method for making the above-described porous metal vacuum molds, embossing rolls, embossing plates, etc.
The objects of the present invention are achieved, briefly, by means of a porous vacuum mold comprising a composite of a first layer of porous metal and a second layer of metal, the two layers being partially in contact and partially separated by channels communicating with a vacuum source and all surfaces of the composite except for the molding surface of the rst layer being covered with an air-impermeable sealer. The channels of the mold are formed by burning a combustible fiber between the two layers so as to leave open, distinct and well defined channels therebetween.
Other objects and advantages of the present invention can best be understood by a perusal of the following detailed description in conjunction with the drawings in which:
FIG. 1 is a front view showing the application of a first layer of porous metal on a flat embodiment mandrel;
FIG. 2 is a perspective view showing the application of a second layer of porous metal on top of a fabric layer over the first porous metal layer;
FIG. 3 is a sectional front view showing, prior to heating in the oven, the :composite formed of the second porous metal layer, the fabric layer, the first layer and the mandrel;
FIG. 4 is a sectional front View of a segment of the composite after removal of the mandrel and application of a sealer layer;
FIG. 5 is a perspective view of the finished mold and the texture of the top surface thereof;
FIG. 6 is a sectional front view of the finished mold and the thermoplastic sheet material to be molded;
FIG. 7 is a sectional perspective View showing the application of a first layer of porous metal on a roll embodiment mandrel;
FIG. 8 is a sectional perspective view of the structure of the fiber layer (of non-interconnected longitudinal fibers) over the first porous metal layer and its relation with a roll ring;
FIG. 9 is a sectional perspective view showing the application of a second layer of porous metal on top of the fiber layer prior to heating of the oven;
FIG. l is an axially exploded sectional perspective view of the finished mold mounted for rotation on a shaft;
FIG. 11 is a sectional perspective view of the finished mold in operation;
FIG. 12 is a front and top view of a commutator ring;
FIG. 13 is a front and top view of a roll ring;
FIG. 14 is a sectional front view of a roll embodiment produced by the reverse process, and
FIG. 15 is. a sectional front view of the fiat embodiment produced by the reverse process.
Referring now to FIG. 1, the substantially fiat mandrel '10 is suitably a plaster form having the desired surface texture and configuration of the surface of the molded product, i.e., it is a positive of the surface of the desired product. The texture of the mandrel shown consists of a series of grooves 11 and ridges 12; however, choice of the texture and, for that matter, the configuration of the mandrel are matters of choice depending upon the specific product desired. The mandrel 10 is larger than the desired product, the desired product being no longer than the distance between the trim edges 13. These trim edges 13 are either grooves or ridges which define the periphery of the molding area and facilitate the removal of the final product from the mold.
A substantially fiat first layer of porous metal is applied over the top surface of the mandrel 10 in such a way as to conform to the surface of the mandrel 10. This first layer 15 of porous metal is very thin, preferably ranging in depth from about V16 inch to about 1A; inch, and is made up of particles of metal lightly mechanically bonded together. It is very porous and will later serve as the molding surface of the vacuum forming mold. The first layer 15 of porous metal may be applied over the entire surface of the mandrel 10 in the form of molten metal by a flame sprayer 16 or by any of the other conventional techniques for forming porous metal layers, such as applying powdered metals or sintering, including the techniques and sprayers described in Modern Plastics, supra, or any of the following U.S. Patents 2,754,225; 2,772,920; 2,784,029; 2,868,667-provided that such technique does not cause undue weakening of the plaster form being used as a mandrel 10.
Although the use of a plaster form as the mandrel material affords certain advantages to be pointed out later, other conventional mandrel materials may be used such as wood, plastic, etc. Where needed, the mandrel 10 should be provided with a release coat to facilitate its subse'quent removal from the first layer 15 of porous metal. A suitable release coat for a plaster form is a light coating of nylon deposited from a solution of nylon in alcohol, but other conventional release coats may also be used such as silicone releases, etc.
While aluminum is the preferred porous metal because of its low cost, ease of handling, relatively low temperature requirement for spraying, and the resultant lower weight of the end product, other metals such .as low melting steels, bronze, copper, nickel and various alloys may be utilized. When the first layer is applied by the spraying of essentially molten metals, the fiame sprayer 16 must be capable of heating materials to the proper temperature for such spraying.
Referring now to FIGS. 2 and 3, a fabric 20 is placed over and in contact with the entire surface of the first layer 15 of porous metal. The fabric 20 extends over and conforms to the entire top surface. Placement of the fabric can be facilitated by wetting the fabric so that it can be contoured to follow closely the surface. The fabric 20 is suitably an open weave combustible fabric, typically a net having approximately 2 to 8 warp and woof (fill) threads per inch, prefer-ably 3 to 4 threads per inch. Each thread has a diameter of from approximately 1A'- to 1/64 inch, preferably about 1/32 inch, It should be recognized that these limitations are not critical, so long as the fabric is loosely woven.
There are few limitations on the combustible type fabrics used in this invention. Obviously, the fabrics used must be of the type which can be destroyed at temperatures below that which will adversely affect the structure of the porous metal. It is preferred that the material be the type which tends to char or burn readily so as to leave channel voids in the porous metal structure. Cotton, wool and vegetable fiber material, such as woven paper fabrics, are among the preferred materials while synthetic fibers such as nylon (polyamides) are not as desirable because (l) they tend to expand on exposure to the high temperature later required, thereby putting a strain on the mold, and (2) they tend to become fluid in such a way as to clog the walls of the passageways to be formed, thereby reducing the effectiveness of the vacuum system.
A substantially flat second layer 25 of porous metal is then applied, e.g., sprayed, over the entire surface of the fabric 20 and into the interstices thereof, so as to contact the portions of the first layer 15 not directly covered yby the fabric 20. The second layer 25 of porous metal is sprayed to a thickness ranging in minimum thickness from about 3A@ to 1A inch. The result is a total sprayed metal layer (made up of layers 15 and 25) of Iapproximately 1A; to Vs inch minimum thickness having embedded therein an open weave net fabric layer.
Referring now to FIG. 3, the composite structure now consists of a plaster form 10, a first sprayed metal layer 15, and open weave combustible fabric 20, and a second sprayed porous metal layer 25. This composite structure is then placed in an oven 30 and heated at 600 to 750 F. for four hours. Naturally, the temperature and time of this heating step will vary with the particular materials which compose the composite structure. The exact duration and temperature will depend on what is necessary to accomplish the purposes of the heating step. For the particular composite structure described, the heating step accomplishes the following objectives: (a) the fabric is burned or reduced to easily removable ash within the porous mold structure leaving defined, open passageways; (b) the water of hydration present in the plaster is removed at this temperature, thereby weakening the plaster and facilitating later removal of the plaster from the first layer 15 of sprayed metal; and (c) the metal layers (without liquifying) become stress relieved, thereby eliminating internal stresses, and form a strong self-supporting structure around the passageways.
The composite structure is then removed from the oven and the plaster mold is broken away from the first layer 15 of porous metal to reveal a textured molding surface of ridges 43 and grooves 44.
Referring now to FIG. 4, the remaining composite consists of the first layer 15, the second layer 25, and the channels 45 therebetween which were created by combustion of the fabric layer 20. The sides and the back surface of the remaining composite (i.e., the exposed outer areas of the remaining composite which were not in contact with the mandrel 10) are then sealed so as to render them air impermeable and to reinforce the remaining composite permitting it to be handled and used without damage thereto. In the present embodiment, sealing was accomplished by coating the sides and back surface of the remaining composite with a sealer layer 40 of epoxy resin and glass cloth; however, other conventional materials and techniques for sealing surfaces (strengthening them and rendering them air impermeable) may be used instead of, or in addition to, the layer 40 of epoxy resin and glass cloth.
The separation and juxtaposition of `the porous metal layers 15, 25 is maintained both through their stress relieved contacts (at the locations correspondin-g to the former interstices of the fabric) around the passageways 45 and through the supporting effect of the sealing layer 40' on their edges.
Referring now to FIG. 5, vacuum holes 51, called vac holes, are created along the periphery of the molding area (comprised of ridges 43 and grooves 44), but outside of the trim line formed by the trim edges 13, i.e., in 4the scrap area of any thermoplastic sheet formed over the mold surface. The -vac holes 51 extend only through the first layer and may be made by drilling, as with a 50 gauge wire drill, through the first layer 15 of porous metal or by other conventional means well known in the art. The vac holes 51 are used to obtain a quick initial pull down of the material to be molded (to speed up the molding process), but are not an essential part of the structure.
Referring now to FIGS. 5 and 6, a large bore and preferably thick-Walled tube 50 is attached to the back or rear surface of the porous -rnold structure and makes an air-impermeable contact with the sealer layer 40. The large bore hole 60 extending through Ithe second layer 25 is suitably made by drilling a W16 inch hole through the second porous metal layer, or by masking portions of the volume to be sprayed with metal to form the second layer. The large bore hole 60 communicates with the tube 50 Vand the channels 45 resulting from the combustion of the fabric layer 20. The large bore tube 50 is fitted with switching means (not shown) for connecting the large bore hole 60 alternately with a vacuum source (not shown) and a source of greater pressure (not shown)preferably -a-t least atmospheric-as desired for the molding operation and sheet removal operation, respectively. The large bore hole 60` and large bore tube 50 act as communicating means Ibetween the vacuum or pressure source and the channels; the first layer 15 of porous metal, in turn, acts as communicating means for vacuum or pressure between the channels and the top surface of the porous mold structure to prevent air entrapment and facilitate sheet removal. The large bore hole 60 directly communicates with several of the small vac holes 51 extending tothe top surface of the porous mold structure and communicates with others indirectly by means of the channels. There may be a single large bore hole 60l and large bore tube 50 or there may be a plurality of them. V
Referring to FIG. 6 in particular, a sheet 61, -composed of unvulcanized rubber or a thermoplastic, heat-softenable plastic heated a few degrees beyond its softening point by heat lamps (not shown), is held within a rectangular holding clamp or frame 62 (say of metal). The frame 62 is lowered or the mold is raised to thereby cause the sheet 61 to contact the top or molding surface of the porous mold structure, the molding surface having been preheated by heat lamps (not shown) to about 140 F. to prevent premature cooling of the sheet 61 before molding. The vacuum source creates a vacuum immediately above the molding surface so as to pull the hot plastic sheet 61 into close contact with the molding surface, first contact occurring around the outside edge of the trim line formed by the trim edges 13 as this area is closest to the direct communication of the vacuum acting directly on the sheet 61 through the vac holes 51. This seals the hot plastic sheet 61 around the top surface periphery of the porous mold structure, thereby causing the vacuum then to pull the hot plastic sheet 61 down to the top surface of the molding area within the trim line of the mold structure. The vacuum action takes place through the channels and, in turn, produces a vacuum at the surface ofthe top layer 15 of porous metal, thereby forcing the hot plastic sheet 61 into intimate contact with the top surface of the first layer 15 of porous metal. The Vac holes 51 are therefore useful in causing the original seal of the plastic sheet 61 to the top surface of the first layer 15 of porous metal, so that the vacuum action through the rst layer 15 is especially efficacious. If desired, the vac holes 51 may be connected to a vacuum source dis tinct and separate from the vacuum source acting through the passageways.
Removal of the molded plastic sheet after it has cooled below the softening point (usually Within a matter of seconds) or vulcanized (cured) to hold the texture of the mold is facilitated by the existence of the trim edges 13 (which enable a lifting blade to be easily inserted under the sheet) and may -be further facilitated by disconnecting the large bore tube 50 from the vacuum sources and either venting it to the atmosphere or connecting it to a pressure source to assist in displacement of the plastic sheet from the top porous metal layer 15 of the mold.
Depending upon the nature of the material to be molded and the texture pattern formed by the grooves 11l and ridges 412 of the mandrel 10, the molded product may be used as a mat for automobiles, a cushion surface, a section of the surface for luggage, etc. For the sake of simplicity, the surface of the porous mold structure illustrated in the drawings is relatively flat, but for specific applications it may be of any desired form and configuration.
It should be noted that although second layer 25 is preferably composed of porous metal, like the first porous metal loyer 15, and although the fabric layer 20 preferably is composed of a lattice of fibers so that the channels resulting from combustion of the fibers are interconnecting (rather than not directly interconnecting as when the fibers of the fabric layer are all substantially parallel), the second layer 25 may be non-porous and/ or non-metallic and some or all of the channels 45 may be other than directly interconnecting.
As noted above, it is possible to have a second layer 25 which is composed not of a porous metal, but rather either of a non-porous metal or of a resin of high distortion temperature, such as an epoxy resin, which will not itself burn or distort during combustion of the fabric layer 20, the bers of which have a low ignition point relative to the distortion temperature of the resin. However, if the second layer 25 is composed of an air-impermeable (non-porous) material, be it metal or high distortion temperature resin, it is essential that the second layer 25 does not completely encapsulate the fibers of the fabric layer 20 or the passageways formed by combustion of the fibers will not communicate with the molding surface of the first layer 15 or porous metal. Such a encapsulation is easily avoided by maintaining contact betweenV the fibers and the first layer 15 of porous metal during application of the non-porous second layer 25. When the second layer 25 is composed of such an airimpermeable non-porous material, it can serve both as a second layer 25 and as the portion of the sealer layer 40 which, in the other embodiments, surrounds the exposed outer areas of the second layer 25. It should be noted, however, that a non-porous second layer 25 may interfere with the vacuum draw of certain channels, e.g., those formed at the location of the alternate (lower) warp threads, which it partially surrounds, thereby causing irregularities in the vacuum on the top surface of the porous mold structure. The porous mold structure having two porous metal layers is thereforeL preferred for most, but not all, applications as it allows any portion (top or bottom) of any channel to suck air from the mold interior so as to produce a uniformly distributed vacuum of constant strength over the molding surface.
Y As noted above, although normally and preferably the passageways formed by the Woof (fill) and warp threads will be interconnecting, due to the physical closeness of the wrap threads to the Woof threads, so that a single vacuum source may be conveniently utilized, it is also possible to have the passageways formed by each warp thread and the passageway formed by each Woof (fill) thread integral and unconnected to other passageways as -by combustion of a very loosely woven fabric. Similarly,
it is possible to replace the fabric layer- 20 with a plurality yof non-woven or parallel combustible fibers or strings, so that the passageways formed by the combustion of the ber do not interconnect. In the non-interconnecting embodiments, appropriate means must be provided for connecting each distinct passageway with a vacuum source, as by providing for each passageway a separate large bore hole 60 and vacuum-connected large bore tube 50. However, to insure application of a uniform pressure or vacuum over the entire molding area, it is preferred that the passageways ybe interconnected. The greater the number Iof direct interconnections between channels, the greater is the likelihood of each segment or length of each channel having the same pressure therein.
Referring now to FIG. 7 in order to construct a preferred roll embodiment, the mandrel 10 used is typically, a reinforced, substantially cylindrical plaster shell of rigid form having .an interior surface with a positive of the desired texture of ridges 12 and grooves 11 on it. Such a mandrel 10 may be formed by casting around an existing embossing roll a continuous seamless cylindrical sleeve of an elastic material capable of capturing and retaining the desired texture of the roll, e.g. vinyl plastisol, silicone and polysulfide rubber, etc. (The continuous cylindrical sleeve may also be made flat and later seamed to form a cylinder where the design or texture lends itself to incorporating the seam as part of the design or later editing it out.) The sleeve is then removed from the embossing roll and pulled over a disposable frame with the textured side facing outwards. A reinforced plaster shell may then be poured lover the textured surface to obtain a rigid form having the interior surface with the desired texture. The disposable frame and the plastisol (or other) sleeve :are then removed from the interior of the plaster.
The inner surface of the hollow plaster mandrel 10 is then sprayed with metal, utilizing a flame sprayer 16, to form a substantially cylindrical first layer 15 of porous metal preferably approximately l/l inch thick. Referring now to FIG. 8, Icombustible fibers (preferably of from 1/32 to 1/16 inch in diameter) are then stretched longitudinally on the inner surface of the first layer 15 parallel to the mandrel axis. The fibers 20 lie approximately 1A inch apart and may be held down to the first layer 15 with a small amount of combustible cement (not shown), such as an unloaded rubber cement, an animal glue or a starch solution, which degrades or tends to disintegrate at the stress relieving temperatures used. Either or both ends of the mandrel 10 are outfitted with prefabricated annular roll rings(s) 130 having extending therethrough roll ring channels or holes 131 (as shown in FIG. 13) aligned along the same longitudinal lines as the fibers 20. Each hole has a slightly greater diameter than that of the fibers. The ends 81 of the fibers 20 are then pulled through roll ring channels or holes 131 and knotted or fastened to each other, there being one hole for each fiber end 81.
Referring now to FIG. 9, a substantially cylindrical second layer of porous metal (preferably, though not necessarily, porous) is applied, as by a flame sprayer 16, over and between the fibers so as to contact the exposed portions of the rst layer 15 (the portions not covered by the fibers 20) and the inner sides of the roll rings(s) 130 until the combined minimum thickness of the first and second layers 15, 25 is approximately 1/2 inch. The entire assembly is then heater in an oven to approximately 650 F. to cause (a) the plaster of the mandrel 10 to lose its water `of hydration (to facilitate later removal thereof from the rst layer 15), (b) the sprayed metal in the first and second layers 15, 25 to anneal (thereby removing stresses) 4and (c) the combustible fibers 20 to char or burn out (thereby leaving small 1/16 inch longitudinal channels 45 between the first and second layers). The assembly is then removed from the oven 30, and the plaster of the mandrel 10 is removed from the molding surface of the lirst layer 15 comprising ridges 43 and grooves 44. The remaining composite of first and second layers 15, 25 and roll ring(s) 130 is slightly warmed to facilitate its placement over a nonporous, rotatable roll shaft of suitable diameter which acts las an air-impermeable sealer for the second layer 25 (see FIGS. l0-1l). If only one end `of the mold has been sealed by the use of a non-porous rool ring 130, the other end is sealed with an aim-impermeable sealer layer.
Referring now to FIGS. 1043, the smooth inner face 121 of a non-porous ring commutator 120 is snugly fitted in a face-to-face relationship against the smoothed outer face 135 of the roll ring 130. The roll ring 130 engages one end of the roll for rotation therewith; the outer commutator ring 120 is stationary and fixedly connected to base 112. The inner face 121 of commutator ring 120 has two separate recessed grooves 122, 123. Recess groove 122 is attached to a vacuum source (not shown) by the tube 102; while recess groove 123 is attached to a source of lesser vacuum (not shown) by tube 103 (eg. tube 103 is vented to the atmosphere or is connected to a source of pressure greater than atmospheric). Recess grooves 122, 123 are located for communication with the roll ring channels, i.e., holes 131, which, in turn, communicate with the channels 45 formed by the combustion of the fibers. The roll embodiment so prepared and assembled, as in FIG. l1, will emboss hot thermoplastic material 61 guided by rollers 105 over that portion of its surface to which a vacuum is applied via the internal channels during the vacuum phase, and the thermoplastic material embossed with ridges 46 and grooves 47 will then be removed from the embossing surface of the roll during the venting or pressure phase. The contact times under vacuum or pressure (venting) can be varied by changing the length of the commutator ring recess grooves 122, 123.
In the operation of the roll embodiment of FIG. 11, the fixed commutator ring is positioned in a faceto-face, slidable air-tight manner against the rotating roll ring 130. At any given instant during the rotation of the roll shaft 100, certain of the holes 131 will be lined up with the recess groove 122 and, therefore, vacuum will be applied to sections of the roll connecting with those particular channels 45 aligned with said holes 131, thereby assisting the embossing. Upon further rotation of the roll, these channels 45 and their corresponding holes 131 will become lined up with the recess groove 123 and will be pressurized or vented to the atmosphere, thereby facilitating stripping of the embossed material from those sections of the roll. To summarize, in order to avoid the difficulty involved in stripping the embossed material from the roll when vacuum is applied to all portions of the roll during a complete 360 rotation, the Vacuum is applied to any section of the porous metal vacuum embossing roll only through approximately 270 or some analogous portion of its rotation and pressure or venting is applied during the remainder of the rotation cycle. This system of roll ring and commutator ring 120 in the roll embodiment therefore corresponds to the switching mechanism in the flat embodiment first described which connects the large bore tube 50 alternately to either a vacuum source or a pressure (or venting) source. It is important to note that, whereas the passageways formed in the at embodiment (by combustion of a woven or nonwoven fabric) may or may not be interconnecting, the passageways formed in the roll embodiment (by combustion of parallel longitudinal fibers) are preferably not interconnecting as it is desired to apply, at any given instant, pressure (or venting) to one set of these channels and vacuum to another set of channels.
Because of the difficulties occasionally encountered in tightly fitting the second layer 25 of the roll embodiment over the non-porous, rotatable roll shaft 100, in certain situations it has been found desirable to use a spider-type shaft to avoid the need for boring out the inner surface of the second layer 25 to insure an exact fit between such inner surface and the outer wall or surface of the rotatable roll shaft 100. The spider-type shaft is a rotatable roll shaft having a diameter considerably smaller than the inner surface of theV second layer 25 and radial or spider arms extending radially therefrom. Because such a spider-type shaft would not be in complete airexcluding contact with the inner surface of the second layer 25, it is necessary to coat the inner surface of the second layer 25 with an air-impermeable sealer layer corresponding to air-impermeable sealer layer 40. As can easily be envisioned, it is a simple matter to insert the radially armed shaft into the hollow formed by the inner surface of the sealer layer on the second layer 25 and then anchor the outer tips of the radial arms to points on the inner surface of the air-impermeable sealer layer with a suitable cement, e.g., epoxy resin. If desired, the radial arms may be hollow and in sufficient number so that each single radial arm connects with a corresponding single longitudinal channel or passageway. In this case, each single hollow radial arm may be caused (as by the boring of appropriately located holes through the second layer) to communicate at the outer tip directly with the corresponding single open passageway and, at another point along its length, with a commutator ring of the type earlier described and shown in FIGS. 12 and 13 of the drawings. In this last variant, therefore, the pressures and Vacuums are distributed by the commutator system to the appropriate longitudinal hollow passageways by means of the hollow radial arms rather than through the roll rings 130, which may therefore be dispensed with.
In any embodiment, cooling means may be provided to accelerate the cooling and hardening of the hot plastic material after molding. Any conventional cooling means may be used, either external or internal to the mold. For internal cooling, tubes for the conduction of water or forced air drafts may be located, for instance, in the second layer 25 of any embodiment or in the shaft 100 of the roll embodiment.
If desired, in any embodiment, the surface of the plaster mandrel contacting the first layer 15 may be smooth, i.e., without any grooves 11 or ridges 12, so that the molding area produced is smiliarly smooth. After the oven heating and removal of the mandrel 10, the first layer 1S may vbe engraved with the desired texture by standard engraving techniques. If the engraving solution plugs the porosity of the first layer 15, then the molding surface thereof may be blasted with water and/ or slightly etched with solvents to recapture the porosity.
For any embodiment, the process for building the mold may be reversed. For the reverse roll embodiment shown in FIG. 14, the outer surface of a mandrel which may be a rotatable shaft 100 (equipped with journals and a water cooled interior) is blasted to receive and hold metal. The second layer 25A of metal is then applied, e.g., sprayedonto the blasted surface to a thickness of 1/s inch. Either the shaft 100 or the second metal layer 25A is non-porous (air-impermeable). Longitudinal fibers are fixed to the surface of the second layer 25A with a suitable combustible cement (not shown) such as animal glue or a starch solution. Roll rings 130 are fixed to the ends of the second layer A over the shaft 100 and the ends of the fibers 20 are fastened through holes 131. The first layer 15A of porous metal is sprayed over the fibers 20, the exposed areas of the second layer 25A of porous metal, and the roll rings 130 to obtain a completely smooth surface (or one that can be so smoothed) having approximately $66 inch of sprayed metal over the fibers. The whole assembly is then heated at 650 F. in an oven to anneal the metal layers 15A, 25A and also burn or char out the fibers 20. The outer or molding surface is next engraved with a negative of the desired texture of grooves 44 and ridges 43 by standard engraving technique methods, the molding surface being waterblasted and/or slightly etched to re-open the first layer 15A if the engraving solution plugs the porosity of the metal. The assembly is then equipped with a commutator 10V ring 120, which is attached to fixed base 112 and has separate recess grooves 122, 123 communicating, respectively, With vacuum and pressure sources by means of tubes 102, 103. The roll is then ready for use as described above.
Sirnilarly, the procedure for the formation of the fiat embodiment may be reversed. Referring now to FIG. 15, the second layer 25A of porous metal is sprayed over a non-porous support 40A corresponding to thel sealer layer 40 (FIG. 6) at the base of the mold. (Alternatively, a non-porous second metal layer may be applied over a release-treated removable surface.) Woven or non-Woven fabric is applied over the second layer 25A. The first layer 15A is then sprayed over the fabric and exposed portions of the second layer 25A. The thickness of the first layer 15A is appropriately adjusted to allow for any diminution thereof due to the subsequent texturing by standard engraving techniques. After heating the above composite at about 650 F., a sealer layer 40B (corresponding to the sealer layer 40 (FIG. 6) at the edges of the mold) is applied around the edges of the first and second layers 15A, 25A. The vac holes 51 and large bore hole 60 are drilled, and large bore tube 50 is inserted and connected to vacuum and pressure sources. After engraving of the first layer 15A with a negative of the desired texture of grooves 44 and ridges 43, the mold is then ready for use as described above.
Of course, many modifications of the specific processes and devices described above may now become apparent to thoselskilled in the art. For instance, the use of a flat type porous vacuum mold to replace at least one part, say the lower half, of a closed or multipiece molding system (of the type conventionally used in the production of latex foam rubber products, such as cushions and bucket seats for automobiles) produces a novel molding system having several distinct advantages over the conventional closed molding system composed of non-porous materials. Because the pores of the porous metal molding surface are finely grained, rubber and chemical plate-out cannot penetrate or clog them, yet gases and moisture can be extracted from the closed molding cavity by them so as to thereby (l) avoid air traps which cause incomplete fill-out of the mold, (2) ensure conformity of the molding compound to the molding cavity because the vacuum on the inner surfaces of the cavity prevents pull-away of the compound therefrom, (3) allow faster cures because steam introduced into the cavity will be pulled through the compound and out of the cavity by the vacuum under the molding surface, and (4) eliminate the need for overflow or vacuuming vents on the mold so that products may be molded without flash, overflow or sprue formation (thereby eliminating the usual waste of molding compound as Well as the usual need for trimming). Consequently, the scope of the instant invention should not be considered as defined by the foregoing disclosure, but by the appended claims.
Having thus described our invention, what we claim and desire to protect by Letters Patent is:
1. As an intermediate article of manufacture suitable for conversion to a device for imparting a predetermined shape to an impressionable material, an object comprising: a layer of porous metal having a shape-imparting surface and a back surface, a supporting layer of metal adjoining said back surface, a plurality of combustible fibers interposed between the adjacent surfaces of said layers, said layers being bonded together in the interstices between said fibers.
2. As an intermediate article of manufacture suitable for conversion to a mold by the application of heat, an object comprising: a porous layer of sprayed metal having a shape-imparting surface and a back surface, a supporting layer of metal adjoining said back surface, a layer of open-weave combustible fabric interposed between said back surface and the adjoining surface of said supporting 3,336,181 11' 12 layer, said porous layer and said supporting layer being References Cited rrnly bonded together in the interstices of said open- UNITED STATES PATENTS weave fabric.
threads, respectively per inch, each thread being from onesixty-fourth (im) inch to one-eighth (M3) inch in di- ALEXANDER WYMAN Primary Examiner ameter. M. A. LITMAN, Examiner.
Claims (1)
- 2. AS AN INTEMEDIATE ARTICLE OF MANUFACTURE SUITABLE FOR CONVERSION TO A MOLD BY THE APPLICATION OF HEAT, AN OBJECT COMPRISING: A POROUS LAYER OF SPRAYED METAL HAVING A SHAPE-IMPARTING SURFACE AND A BACK SURFACE, A SUPPORTING LAYER OF METAL ADJOINING SAID BACK SURFACE, A LAYER OF OPEN-WEAVE COMBUSTIBLE FABRIC INTERPOSED BETWEEN SAID BACK SURFACE AND THE ADJOINING SURFACE OF SAID SUPPORTING LAYER, SAID POROUS LAYER AND SAID SUPPORTING LAYER BEING FIRMLY BONDED TOGETHER IN THE INTERSTICES OF SAID OPENWEAVE FABRIC.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US53743666 US3336181A (en) | 1963-05-22 | 1966-03-25 | Molding apparatus and process for making the same |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US282443A US3262159A (en) | 1963-05-22 | 1963-05-22 | Molding apparatus and process for making same |
US484043A US3293737A (en) | 1963-05-22 | 1965-08-31 | Process for making mold for vacuum-forming materials |
US53743666 US3336181A (en) | 1963-05-22 | 1966-03-25 | Molding apparatus and process for making the same |
Publications (1)
Publication Number | Publication Date |
---|---|
US3336181A true US3336181A (en) | 1967-08-15 |
Family
ID=27403309
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US53743666 Expired - Lifetime US3336181A (en) | 1963-05-22 | 1966-03-25 | Molding apparatus and process for making the same |
Country Status (1)
Country | Link |
---|---|
US (1) | US3336181A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3492720A (en) * | 1965-11-09 | 1970-02-03 | Basf Ag | Production of porous electrodes |
US5817267A (en) * | 1995-11-13 | 1998-10-06 | General Magnaplate Corporation | Fabrication of tooling by thermal spraying |
US20060097423A1 (en) * | 2004-10-12 | 2006-05-11 | General Magnaplate Corporation | Light weight spray tooling |
US20060210718A1 (en) * | 2005-03-21 | 2006-09-21 | General Magnaplate Corporation | Combination high density/low density layers |
US20060266472A1 (en) * | 2005-05-06 | 2006-11-30 | Kipp Michael D | Vacuum bagging methods and systems |
US7270167B1 (en) * | 2004-12-03 | 2007-09-18 | Gmic Corp. | Metal impregnated graphite composite tooling |
US20080008836A1 (en) * | 2006-05-01 | 2008-01-10 | Kipp Michael D | Method for extending the useful life of mold type tooling |
US20080105997A1 (en) * | 2006-10-17 | 2008-05-08 | Ridges Michael D | Method for enhancing the sealing potential of formable, disposable tooling materials |
US20080106007A1 (en) * | 2006-10-17 | 2008-05-08 | Kipp Michael D | Resin infusion process utilizing a reusable vacuum bag |
US20080131716A1 (en) * | 2006-12-04 | 2008-06-05 | American Consulting Technology & Research, Inc. | Shrinkable film barrier for mandrel tooling members |
US20080182054A1 (en) * | 2007-01-09 | 2008-07-31 | Ridges Michael D | Multi-function vacuum bag for composite part manufacture |
US8313600B2 (en) | 2008-08-15 | 2012-11-20 | Sigma-Tek, Llc | Method and system for forming composite geometric support structures |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2860175A (en) * | 1955-09-05 | 1958-11-11 | Ruhrchemie Ag | Homeoporous gas-diffusion electrode for galvanic cells |
US2873219A (en) * | 1954-12-20 | 1959-02-10 | Joseph B Brennan | Metal-coated batt and method and apparatus for producing same |
US3228798A (en) * | 1962-04-12 | 1966-01-11 | Electric Storage Battery Co | Gas electrode |
-
1966
- 1966-03-25 US US53743666 patent/US3336181A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2873219A (en) * | 1954-12-20 | 1959-02-10 | Joseph B Brennan | Metal-coated batt and method and apparatus for producing same |
US2860175A (en) * | 1955-09-05 | 1958-11-11 | Ruhrchemie Ag | Homeoporous gas-diffusion electrode for galvanic cells |
US3228798A (en) * | 1962-04-12 | 1966-01-11 | Electric Storage Battery Co | Gas electrode |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3492720A (en) * | 1965-11-09 | 1970-02-03 | Basf Ag | Production of porous electrodes |
US5817267A (en) * | 1995-11-13 | 1998-10-06 | General Magnaplate Corporation | Fabrication of tooling by thermal spraying |
US20060097423A1 (en) * | 2004-10-12 | 2006-05-11 | General Magnaplate Corporation | Light weight spray tooling |
US7270167B1 (en) * | 2004-12-03 | 2007-09-18 | Gmic Corp. | Metal impregnated graphite composite tooling |
US20060210718A1 (en) * | 2005-03-21 | 2006-09-21 | General Magnaplate Corporation | Combination high density/low density layers |
US20060266472A1 (en) * | 2005-05-06 | 2006-11-30 | Kipp Michael D | Vacuum bagging methods and systems |
US20080008836A1 (en) * | 2006-05-01 | 2008-01-10 | Kipp Michael D | Method for extending the useful life of mold type tooling |
US20080105997A1 (en) * | 2006-10-17 | 2008-05-08 | Ridges Michael D | Method for enhancing the sealing potential of formable, disposable tooling materials |
US20080106007A1 (en) * | 2006-10-17 | 2008-05-08 | Kipp Michael D | Resin infusion process utilizing a reusable vacuum bag |
US20080131716A1 (en) * | 2006-12-04 | 2008-06-05 | American Consulting Technology & Research, Inc. | Shrinkable film barrier for mandrel tooling members |
US20080182054A1 (en) * | 2007-01-09 | 2008-07-31 | Ridges Michael D | Multi-function vacuum bag for composite part manufacture |
US8313600B2 (en) | 2008-08-15 | 2012-11-20 | Sigma-Tek, Llc | Method and system for forming composite geometric support structures |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3336181A (en) | Molding apparatus and process for making the same | |
US2420522A (en) | Method of making articles from plastic treated materials | |
US3135640A (en) | Process of and an apparatus for manufacturing hollow articles from reinforced synthetic resins | |
US2441097A (en) | Plastics molding apparatus | |
US4946640A (en) | Method for forming preformed material | |
US4551297A (en) | Method of making an embossing cylinder | |
US1592536A (en) | Pneumatic forming and holding of rubber | |
US2838435A (en) | Method of forming plastic parts | |
US4042433A (en) | Appliqueing synthetic resins on sheet material | |
US2532442A (en) | Molded article | |
US3262159A (en) | Molding apparatus and process for making same | |
US3293737A (en) | Process for making mold for vacuum-forming materials | |
GB2167014A (en) | Embossing | |
US4874448A (en) | Method of making seat-like object | |
US2781078A (en) | Apparatus for vacuum forming ductile material | |
US2345112A (en) | Method of molding plastic layers | |
EP0227753B1 (en) | Rapid moulding of hollow elongate concrete articles | |
US3018540A (en) | Methods for making embossing rollers | |
US3041668A (en) | Methods for forming sheet plastics | |
US2359948A (en) | Method of making dipped rubber articles | |
SE8203842D0 (en) | SET AND DEVICE FOR MANUFACTURE OF NECK BODIES IN REINFORCED RESIN, SPECIAL PROTECTIVE HELMETS | |
US3205288A (en) | Method of manufacture of hollow reinforced plastic articles | |
US1846279A (en) | Means for molding articles from alpha slip or plastic mass | |
US4216043A (en) | Embossed patterning of asbestos-cement and like sheets | |
US3205123A (en) | Method and apparatus for applying a plastic sheet to a pulp molded article on the mold |